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6110 Aluminum vs. SAE-AISI 1552 Steel

6110 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1552 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is SAE-AISI 1552 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2
11 to 14
Fatigue Strength, MPa 120
290 to 400
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 290
460 to 510
Tensile Strength: Ultimate (UTS), MPa 500
760 to 840
Tensile Strength: Yield (Proof), MPa 500
460 to 650

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 600
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 170
51
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
11
Electrical Conductivity: Equal Weight (Specific), % IACS 140
12

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
1.8
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1170
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
81 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
560 to 1130
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 51
27 to 30
Strength to Weight: Bending, points 51
24 to 25
Thermal Diffusivity, mm2/s 67
14
Thermal Shock Resistance, points 22
26 to 29

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
0
Carbon (C), % 0
0.47 to 0.55
Chromium (Cr), % 0.040 to 0.25
0
Copper (Cu), % 0.2 to 0.7
0
Iron (Fe), % 0 to 0.8
97.9 to 98.3
Magnesium (Mg), % 0.5 to 1.1
0
Manganese (Mn), % 0.2 to 0.7
1.2 to 1.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.7 to 1.5
0
Sulfur (S), % 0
0 to 0.050
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0